DE60301117D1 - Methode und Vorrichtung für dynamischen Ausgleich mit Reaktionsrädern während einer länger dauernden Entfaltung eines grossen Reflektors - Google Patents

Methode und Vorrichtung für dynamischen Ausgleich mit Reaktionsrädern während einer länger dauernden Entfaltung eines grossen Reflektors

Info

Publication number
DE60301117D1
DE60301117D1 DE60301117T DE60301117T DE60301117D1 DE 60301117 D1 DE60301117 D1 DE 60301117D1 DE 60301117 T DE60301117 T DE 60301117T DE 60301117 T DE60301117 T DE 60301117T DE 60301117 D1 DE60301117 D1 DE 60301117D1
Authority
DE
Germany
Prior art keywords
dynamic compensation
wheels during
reaction wheels
large reflector
longer deployment
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
DE60301117T
Other languages
English (en)
Other versions
DE60301117T2 (de
Inventor
Hanching Grant Wang
Richard A Fowell
Che-Hang C Ih
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Boeing Co
Original Assignee
Boeing Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Boeing Co filed Critical Boeing Co
Publication of DE60301117D1 publication Critical patent/DE60301117D1/de
Application granted granted Critical
Publication of DE60301117T2 publication Critical patent/DE60301117T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/283—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using reaction wheels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/244—Spacecraft control systems
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/285—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using momentum wheels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/26—Guiding or controlling apparatus, e.g. for attitude control using jets
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/281—Spin-stabilised spacecraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • B64G1/361—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using star sensors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • B64G1/363—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using sun sensors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • B64G1/366—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using magnetometers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • B64G1/369—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using gyroscopes as attitude sensors

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
DE60301117T 2002-12-13 2003-12-11 Methode und Vorrichtung für dynamischen Ausgleich mit Reaktionsrädern während einer länger dauernden Entfaltung eines grossen Reflektors Expired - Lifetime DE60301117T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US318867 2002-12-13
US10/318,867 US6990396B2 (en) 2002-12-13 2002-12-13 Method and apparatus for reaction wheel dynamic compensation in long-duration deployment of a large reflector

Publications (2)

Publication Number Publication Date
DE60301117D1 true DE60301117D1 (de) 2005-09-01
DE60301117T2 DE60301117T2 (de) 2006-06-08

Family

ID=32325982

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60301117T Expired - Lifetime DE60301117T2 (de) 2002-12-13 2003-12-11 Methode und Vorrichtung für dynamischen Ausgleich mit Reaktionsrädern während einer länger dauernden Entfaltung eines grossen Reflektors

Country Status (4)

Country Link
US (1) US6990396B2 (de)
EP (1) EP1428754B1 (de)
JP (1) JP4969020B2 (de)
DE (1) DE60301117T2 (de)

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US7149610B2 (en) * 2003-08-26 2006-12-12 The Boeing Company Momentum estimator for on-station momentum control
US7185858B2 (en) * 2003-11-26 2007-03-06 The Boeing Company Spacecraft gyro calibration system
US7665695B2 (en) * 2003-12-03 2010-02-23 The Boeing Company Unified attitude control for spacecraft transfer orbit operations
US20050133670A1 (en) * 2003-12-03 2005-06-23 Wang H. G. Unified sensor-based attitude determination and control for spacecraft operations
US20080099626A1 (en) * 2006-10-27 2008-05-01 Goodrich Corporation Reconfigurable reaction wheel for spacecraft
CN102012490B (zh) * 2009-09-08 2013-05-22 上海卫星工程研究所 一种星载磁强计的支架结构
US8561944B2 (en) * 2010-06-17 2013-10-22 Lockheed Martin Corporation System and method for desaturation of a control moment gyroscope
US8800935B2 (en) * 2011-03-09 2014-08-12 Space Systems/Loral, Llc Spacecraft payload positioning with respect to a virtual pivot point
FR2993863B1 (fr) * 2012-07-27 2014-08-29 Thales Sa Procede de reduction du moment cinetique et de controle d'attitude d'un engin spatial
FR3010053B1 (fr) * 2013-08-30 2016-10-21 Thales Sa Procede et dispositif de propulsion electrique de satellite
US9764858B2 (en) * 2015-01-07 2017-09-19 Mitsubishi Electric Research Laboratories, Inc. Model predictive control of spacecraft
US9889950B2 (en) 2015-02-20 2018-02-13 Space Systems/Loral, Llc Spacecraft with aerodynamic control
KR101640720B1 (ko) * 2015-12-17 2016-07-18 한국항공우주연구원 위성 자세 제어 성능 비교 방법 및 장치
CN106383523B (zh) * 2016-09-30 2019-03-08 湖北航天技术研究院总体设计所 一种飞行器非线性姿态控制***稳定性分析方法
IT201900019322A1 (it) * 2019-10-18 2021-04-18 Thales Alenia Space Italia Spa Con Unico Socio Assistenza end-to-end in orbita
CN111017268B (zh) * 2019-12-09 2022-06-24 上海航天控制技术研究所 一种空间站对称舱段太阳翼协同控制***及其控制方法
KR20230155576A (ko) * 2021-03-16 2023-11-10 에이에스티 앤 사이언스, 엘엘씨 우주 내 물체를 위한 운동량 휠 및 반동 휠
CN113536550B (zh) * 2021-06-29 2024-01-12 中国人民解放军63920部队 态势图生成方法、装置、非易失性存储介质及处理器

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4325124A (en) 1979-02-28 1982-04-13 Organisation Europeenne De Recherches Spatiales System for controlling the direction of the momentum vector of a geosynchronous satellite
US4306692A (en) 1979-03-16 1981-12-22 Communications Satellite Corporation Attitude acquisition maneuver for a bias momentum spacecraft
JPS63125498A (ja) * 1986-11-14 1988-05-28 三菱電機株式会社 人工衛星の姿勢制御装置
JPH01275300A (ja) * 1988-04-28 1989-11-02 Nec Corp 太陽輻射圧による宇宙飛翔体の姿勢制御法
US4949922A (en) 1988-12-09 1990-08-21 Hughes Aircraft Company Satellite control system
FR2669887B1 (fr) * 1990-11-30 1995-06-02 Aerospatiale Procede de controle d'attitude en tangage d'un satellite grace a la pression de radiation solaire et satellite adapte a sa mise en óoeuvre.
JPH0717496A (ja) * 1993-07-07 1995-01-20 Fujitsu Ltd 人工衛星の姿勢制御方式
US6017000A (en) 1998-08-02 2000-01-25 Scott; David R. Apparatus and methods for in-space satellite operations
JP3366095B2 (ja) * 1994-02-10 2003-01-14 宇宙開発事業団 人工衛星の外乱トルク推定装置
US5816540A (en) 1995-12-22 1998-10-06 Hughes Electronics Optimal solar tracking system
US5906339A (en) 1996-11-07 1999-05-25 Motorola, Inc. Multiple axis solar sailing
US6032903A (en) 1998-02-12 2000-03-07 Hughes Electronics Corporation Cooperative control structures and methods for satellite spin axis control
US6138953A (en) * 1998-03-02 2000-10-31 Hughes Electronics Corporation Slew rate direction determination for acquisition maneuvers using reaction wheels
US6076773A (en) 1998-04-10 2000-06-20 Hughes Electronics Corporation Spin-stabilized spacecraft and methods
US6463365B1 (en) 2000-02-01 2002-10-08 Raytheon Company System and method for controlling the attitude of a space craft

Also Published As

Publication number Publication date
EP1428754B1 (de) 2005-07-27
US20040117074A1 (en) 2004-06-17
US6990396B2 (en) 2006-01-24
EP1428754A1 (de) 2004-06-16
JP2004196290A (ja) 2004-07-15
JP4969020B2 (ja) 2012-07-04
DE60301117T2 (de) 2006-06-08

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